CN107600319A - A kind of return capsule operating platform - Google Patents
A kind of return capsule operating platform Download PDFInfo
- Publication number
- CN107600319A CN107600319A CN201710846231.8A CN201710846231A CN107600319A CN 107600319 A CN107600319 A CN 107600319A CN 201710846231 A CN201710846231 A CN 201710846231A CN 107600319 A CN107600319 A CN 107600319A
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- China
- Prior art keywords
- return capsule
- air bag
- operating platform
- deck
- return
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Abstract
The present invention relates to a kind of return capsule operating platform, including return capsule mounting, two movable operation platforms；Return capsule mounting is fixedly installed on the deck of ship, has rubber blanket in the middle part of return capsule mounting, air bag cushion is provided with the outside of rubber blanket, and external diameter is sequentially provided with the outside of air bag cushion and arrives at least two big air bag rings from childhood；Guide rail is fixed with the deck of return capsule mounting both sides；Movable operation platform includes being used for the conjunction frame in semicircular configuration for blocking return capsule external diameter, closes and is supported below frame by supporting construction, supporting construction bottom is slidably matched with guide rail；Supporting construction is provided with inclined ladder；The both sides of the ladder of one of movable operation platform are be hinged to set the baffle plate that can be overturn to middle part, and slide is formed after baffle plate turning.The present invention completes return capsule, and spacefarer conveniently goes out the processes such as cabin, the convenient operation of staff after timely salvaging under high sea conditions, and reaches equipment dismounting simplicity, and contract short-period purpose.
Description
Technical field
The present invention relates to a kind of return capsule operating platform, belong to Space Equipment technical field.
Background technology
Return capsule is also known as cockpit, and it is spacefarer's " driver's cabin ".It is that spacefarer comes and goes the bay section taken during space, is close
Structure is closed, there is hatch door front end.Region residing for spacefarer during return, in addition to being equipped with and can reduce the seat of impulsive force, spacefarer
Emergency article and instrument, film, tape, test specimen and science data and remote sensing data etc. can all be placed on here.Return
Cabin is most important part in space launch system, directly ensures the life and instrument and equipment safety of spacefarer.With this
Also outer celestial body sample and data are taken back simultaneously the sole support of the earth.
Existing return capsule, after salvaging to deck, the convenience that the stationarity of placement and astronaut go out cabin is all present
Certain deficiency, especially under high sea conditions there is certain difficulty in the process such as spacefarer's export, staff's operation.
The content of the invention
The technical problem to be solved in the invention is：Existing return capsule, after salvaging to deck, the stationarity of placement,
And certain deficiency all be present in the convenience that astronaut goes out cabin, spacefarer's export, staff especially under high sea conditions
Certain difficulty be present in the processes such as operation.
The present invention takes following technical scheme：
A kind of return capsule operating platform, including 4, two movable operation platforms 2 of return capsule mounting；The return capsule mounting
4 are fixedly installed on the deck 3 of ship, and the middle part of return capsule mounting 4 has rubber blanket 4b, and air bag cushion is provided with the outside of rubber blanket
External diameter is sequentially provided with the outside of 4c, air bag cushion 4c and arrives at least two big air bag ring 4d from childhood；The deck of the both sides of return capsule mounting 4
On be fixed with guide rail 204；The movable operation platform 2 includes being used for the conjunction in semicircular configuration for blocking return capsule external diameter
Frame 201, close the lower section of frame 201 and supported by supporting construction, the supporting construction bottom is slidably matched with the guide rail 204；The branch
Support structure is provided with inclined ladder 202；The both sides of the ladder 202 of one of movable operation platform 2 are hinged setting can be to
The baffle plate 203 of middle part upset, baffle plate 203 form slide after overturning.
Further, the bottom of movable operation platform 2 is provided with the sliding block pad 205 for being used for coordinating with guide rail 204.
Further, the conjunction frame 201 is surrounded by guardrail.
Further, there is ledge structure on the outside of the air bag cushion 4c, minimum air bag ring be stuck in the ledge structure and
Between the bottom of return capsule 1, outermost air bag ring bottom connects one layer of canvas being connected with deck 3, air bag cushion and canvas hasp
Connection, adjacent cells circle by hasp connection, rubber blanket 4b also with canvas hasp connection；Rubber blanket 4b, air bag cushion 4c, air bag ring
4d links together to be fixed by bolt and deck plane.
Further, operating platform floor uses Figured aluminium plate；Guide rail 204 is arranged on channel-section steel, and channel-section steel is with deck in ship
Embody field and carry out spot welding connection.
Further, movable operation platform 2 uses light aluminum alloy material.
The beneficial effects of the present invention are：
1) this return capsule operating platform is easy to assembly all using modularization, parting mode design；
2) operating platform is quick detachable, is easily assembled, usually not the used time can be placed in warehouse be easy to keeping and safeguard；
3) it can be assembled and debugged to quickly complete by 2-3 names staff at work；
4) return capsule mounting employs the pattern that rubber blanket is combined with air bag ring, and rubber blanket can bear heavier return capsule
Weight, size air bag ring and air bag cushion and can control the posture of return capsule well so that the posture that return capsule is kept upright is not
It can fall down；
5) inclement weather conditions of operation on the sea are considered, under 6 grades of sea situations, is not in that platform is mobile, is broken, is curved
Situations such as bent, air bag breakage, can be provided under harsh natural environment for spacefarer and staff safety platform and
Protection；
6) this return capsule operating platform employs symmetrical mentality of designing, compared in the past traditional unilateral stair mould
Formula, greatly improve safety and reliability；
7) unilateral operating platform provides the design structure of slide, and slide can overturn to be formed as needed, it is not necessary to the used time
Fixed after foldable and by ladder side, not only easy but also practical, sufficiently being injured in view of spacefarer needs carrying large instrument
The situation of equipment, substantially increases feature and practicality；
8) this return capsule reclaimer operation platform and return capsule mounting are all using marine aluminium alloy and elastomeric material, with tradition
Ferrous materials reduce 2/3rds compared to not only weight, and substantially increase antiseptic property, under severe sea situation not
Situations such as burn into corrosion can be produced.
Brief description of the drawings
Fig. 1 is the front view of return capsule operating platform of the present invention.
Fig. 2 is the schematic diagram of return capsule and return capsule mounting below.
Fig. 3 be in Fig. 2 A-A to sectional view.
Fig. 4 is the dimensional structure diagram without slide side movable operation platform.
Fig. 5 is the front view with slide side movable operation platform.
Fig. 6 is Fig. 5 top view.
Fig. 7 is Fig. 5 left view.
In figure, 1. return capsules, 2. movable operation platforms, 3. decks, 4. movable operation platforms, 4a. return capsules, 4b.
Rubber blanket, 4c. air bag cushions, 4d. air bag rings, 201. conjunction framves, 202. ladders, 203. baffle plates, 204. guide rails, 205. sliding block pads,
206. first support bars, 207. second support bars.
Embodiment
The present invention is further described with specific embodiment below in conjunction with the accompanying drawings.
In this embodiment, it is removable referring to Fig. 1-7, a kind of return capsule operating platform, including return capsule mounting 4, two
Operating platform 2；The return capsule mounting 4 is fixedly installed on the deck 3 of ship, and the middle part of return capsule mounting 4 has rubber
4b is padded, air bag cushion 4c is provided with the outside of rubber blanket, external diameter is sequentially provided with the outside of air bag cushion 4c and arrives at least two big air bags from childhood
Enclose 4d；Guide rail 204 is fixed with the deck of the both sides of return capsule mounting 4；The movable operation platform 2 includes being used to block to return
The conjunction frame 201 in semicircular configuration of reboard external diameter, close the lower section of frame 201 and supported by supporting construction, the supporting construction bottom with
The guide rail 204 is slidably matched；The supporting construction is provided with inclined ladder 202；One of movable operation platform 2
The both sides of ladder 202 are be hinged to set the baffle plate 203 that can be overturn to middle part, and baffle plate 203 forms slide after overturning.
In this embodiment, it is provided with the cunning for being used for coordinating with guide rail 204 referring to Fig. 5, the bottom of movable operation platform 2
Block pad 205.
In this embodiment, it is surrounded by guardrail referring to Fig. 4-5, the conjunction frame 201.
In this embodiment, there is ledge structure referring to Fig. 3, the air bag cushion 4c outsides, minimum air bag ring is stuck in institute
State between ledge structure and the bottom of return capsule 1, outermost air bag ring bottom connects one layer of canvas being connected with deck 3, air bag cushion
With canvas hasp connection, adjacent cells circle by hasp connection, rubber blanket 4b also with canvas hasp connection；Rubber blanket 4b, gas
Capsule pad 4c, air bag ring 4d link together and fixed by bolt and deck plane.
In this embodiment, operating platform floor uses Figured aluminium plate；Guide rail 204 is arranged on channel-section steel, channel-section steel and deck
Spot welding connection is carried out at hull scene.
In this embodiment, movable operation platform 2 uses light aluminum alloy material.
Movable operation platform 2 is closed configuration or disassembled form usually, by movable operation platform 2 before use
Separated or Quick installation platform, after return capsule is laid steadily in mounting, the operating platform on both sides slowly closes up to form one
Individual overall platform, and fix good position with latch and make it that operating platform is stable and firm.Return capsule operating platform can bear 500KG
Load.And there is enough operation convolution spaces, there is safety guide rail on platform, operating platform floor uses Figured aluminium plate energy
Anti-skidding effect is played, the baffle plate of stair can be turned down to form one with slide, used when being necessary for spacefarer.It is whole
Individual operating platform, which is arranged on guide rail, can easily be promoted by staff, slided.Guide rail is arranged on channel-section steel, channel-section steel and deck
Spot welding connection is carried out at hull scene.Whole system has the characteristics of convenient disassembly, continuous reliable.
Return capsule mounting be made from multiple components including：Air vesicle circle, ballonet circle, air bag cushion and rubber blanket and connection
Part etc..Wherein air vesicle circle bottom connects one layer of canvas and is used to connect with deck, air bag cushion and bottom canvas hasp connection, stingy
Nang Quan and air vesicle circle by hasp connection, rubber blanket also with bottom canvas hasp connection.All seat components are connected to one
Rise and fixed by bolt and deck plane so that the weight for bearing return capsule above deck that mounting can be stable.
The present invention completes return capsule, and spacefarer conveniently goes out cabin after salvaging in time under high sea conditions, staff conveniently grasps
The processes such as work, and reach equipment dismounting simplicity, contract short-period purpose.
Above is the preferred embodiments of the present invention, those of ordinary skill in the art can also carry out various changes on this basis
Change or improve, on the premise of the total design of the present invention is not departed from, these conversion or improvement should all belong to application claims guarantor
Within the scope of shield.
Claims (6)
- A kind of 1. return capsule operating platform, it is characterised in that：Including return capsule mounting (4), two movable operation platforms (2)；The return capsule mounting (4) is fixedly installed on the deck (3) of ship, has rubber in the middle part of the return capsule mounting (4) Pad (4b), air bag cushion (4c) is provided with the outside of rubber blanket, external diameter is sequentially provided with the outside of air bag cushion (4c) and arrives big at least two from childhood Individual air bag ring (4d)；Guide rail (204) is fixed with the deck of return capsule mounting (4) both sides；The movable operation platform (2) includes being used for the conjunction frame (201) in semicircular configuration for blocking return capsule external diameter, closes frame (201) lower section is supported by supporting construction, and the supporting construction bottom is slidably matched with the guide rail (204)；The supporting construction It is provided with inclined ladder (202)；The both sides of the ladder (202) of one of movable operation platform (2) are be hinged to set the baffle plate that can be overturn to middle part (203), slide is formed after baffle plate (203) upset.
- 2. return capsule operating platform as claimed in claim 1, it is characterised in that：Movable operation platform (2) bottom is set There is the sliding block pad (205) for coordinating with guide rail (204).
- 3. return capsule operating platform as claimed in claim 1, it is characterised in that：The conjunction frame (201) is surrounded by guardrail.
- 4. return capsule operating platform as claimed in claim 1, it is characterised in that：There is Step-edge Junction on the outside of the air bag cushion (4c) Structure, minimum air bag ring are stuck between ledge structure and return capsule (1) bottom, outermost air bag ring bottom connect one layer with The canvas of deck (3) connection, air bag cushion and canvas hasp connection, adjacent cells circle by hasp connection, rubber blanket (4b) also with Canvas hasp connection；Rubber blanket (4b), air bag cushion (4c), air bag ring (4d) link together and consolidated by bolt and deck plane It is fixed.
- 5. return capsule operating platform as claimed in claim 1, it is characterised in that：Operating platform floor uses Figured aluminium plate；Lead Rail (204) is arranged on channel-section steel, and channel-section steel carries out spot welding at hull scene with deck and is connected.
- 6. return capsule operating platform as claimed in claim 1, it is characterised in that：Movable operation platform (2) is using light Aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710846231.8A CN107600319B (en) | 2017-09-19 | 2017-09-19 | Return cabin operation platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710846231.8A CN107600319B (en) | 2017-09-19 | 2017-09-19 | Return cabin operation platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107600319A true CN107600319A (en) | 2018-01-19 |
| CN107600319B CN107600319B (en) | 2023-08-15 |
Family
ID=61061321
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710846231.8A Active CN107600319B (en) | 2017-09-19 | 2017-09-19 | Return cabin operation platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107600319B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116692040A (en) * | 2023-07-11 | 2023-09-05 | 西安四方超轻材料有限公司 | Return cabin recycling operation platform |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4832288A (en) * | 1987-07-23 | 1989-05-23 | Aerospace Recovery System, Inc. | Recovery system |
| JPH04287800A (en) * | 1991-03-18 | 1992-10-13 | Ishikawajima Harima Heavy Ind Co Ltd | Unloading method for payload |
| US6237875B1 (en) * | 1998-08-18 | 2001-05-29 | Daimlerchrysler Ag | Airbag payload landing system for damping landing impact forces on a flying payload |
| CN1978279A (en) * | 2005-12-05 | 2007-06-13 | 罗进南 | Efficient flying boat and missile with tail-wing-skirt self-stabilizing return capsule |
| CN200939940Y (en) * | 2006-06-26 | 2007-08-29 | 董兰田 | Shock-absorber for returning-back cabin of spaceship during its landing to the earth |
| CN101704407A (en) * | 2009-11-19 | 2010-05-12 | 哈尔滨工业大学 | Maritime emergent floating bag life-saving system for re-entry capsule |
| CN101857077A (en) * | 2010-04-27 | 2010-10-13 | 中国水产科学研究院渔业机械仪器研究所 | Marine fixed seat frame structure of reentry module |
| WO2014021744A2 (en) * | 2012-07-31 | 2014-02-06 | Aleksandrov Oleg Aleksandrovich | Method for putting ring-shaped and grid-like surfaces into outer space and a device for implementing same |
| CN106114916A (en) * | 2016-08-12 | 2016-11-16 | 哈尔滨工业大学 | A kind of inflating expanded periodicity capsule flap-type decelerator and curling thereof fold gathering method |
-
2017
- 2017-09-19 CN CN201710846231.8A patent/CN107600319B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4832288A (en) * | 1987-07-23 | 1989-05-23 | Aerospace Recovery System, Inc. | Recovery system |
| JPH04287800A (en) * | 1991-03-18 | 1992-10-13 | Ishikawajima Harima Heavy Ind Co Ltd | Unloading method for payload |
| US6237875B1 (en) * | 1998-08-18 | 2001-05-29 | Daimlerchrysler Ag | Airbag payload landing system for damping landing impact forces on a flying payload |
| CN1978279A (en) * | 2005-12-05 | 2007-06-13 | 罗进南 | Efficient flying boat and missile with tail-wing-skirt self-stabilizing return capsule |
| CN200939940Y (en) * | 2006-06-26 | 2007-08-29 | 董兰田 | Shock-absorber for returning-back cabin of spaceship during its landing to the earth |
| CN101704407A (en) * | 2009-11-19 | 2010-05-12 | 哈尔滨工业大学 | Maritime emergent floating bag life-saving system for re-entry capsule |
| CN101857077A (en) * | 2010-04-27 | 2010-10-13 | 中国水产科学研究院渔业机械仪器研究所 | Marine fixed seat frame structure of reentry module |
| WO2014021744A2 (en) * | 2012-07-31 | 2014-02-06 | Aleksandrov Oleg Aleksandrovich | Method for putting ring-shaped and grid-like surfaces into outer space and a device for implementing same |
| CN106114916A (en) * | 2016-08-12 | 2016-11-16 | 哈尔滨工业大学 | A kind of inflating expanded periodicity capsule flap-type decelerator and curling thereof fold gathering method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116692040A (en) * | 2023-07-11 | 2023-09-05 | 西安四方超轻材料有限公司 | Return cabin recycling operation platform |
| CN116692040B (en) * | 2023-07-11 | 2024-04-26 | 西安四方超轻材料有限公司 | Return cabin recycling operation platform |
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| Publication number | Publication date |
|---|---|
| CN107600319B (en) | 2023-08-15 |
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| CB03 | Change of inventor or designer information |
Inventor after: Fang Xiong Inventor after: Jian Zhixin Inventor after: Ye Jianshe Inventor after: Xu Zhiqiang Inventor after: Wang Zhiyong Inventor after: Liu Ping Inventor after: Lin Liqun Inventor after: Shen Xicheng Inventor after: Xi Xiyang Inventor before: Fang Xiong Inventor before: Jian Zhixin Inventor before: Xu Zhiqiang Inventor before: Wang Zhiyong Inventor before: Liu Ping Inventor before: Lin Liqun Inventor before: Shen Xicheng Inventor before: Xi Xiyang |
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